JASC 5350
Service difficulty reports · 6,124
Reports filed under 5350 · Aerodynamic Fairings, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5350' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5350' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA200905261789Fairing · corrodedWING-TO-BODY FAIRING LOWER STRUCTURE HAS CORROSION AT STA 1060, LBL 8.0 INCH TO RBL 8.0 INCH. CORROSION AREA BLENDED AND FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. REPAIR CARRIED OUT ON WING-TO-BODY FAIRING LOWER STRUCTURE IAW SRM 51-70-12 REV. 97. REPAIR ISDR FDEA200905251785Fairing · corrodedWING-TO-BODY FAIRING LOWER STRUCTURE HAS CORROSION AT STA 1060, LBL 8.0 INCH TO RBL 8.0 INCH. REPAIR CARRIED OUT ON WING-TO-BODY FAIRING LWR STRUCTURE AT ST 1060 IAW SRM 51-70-12 FIG 1 DETAIL III REV 97. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIASDR HALA2009051400177Radome · delaminatedDURING ETOPS INSPECTION WALKAROUND FOUND EVIDENCE OF BIRDSTRIKE ON NOSE RADOME AT APPROX 8:00 PO APPROX 12 INCHES FROM CENTER AS VIEWED FROM FRONT OF ACFT. INSPECTED PER BIRD STRIKE INSP IN AMM 05-51-18 FOUND EVIDENCE OF DELAMINATION ON INSIDE OF RADOME FORWASDR DLM88091035Tube · wornWORN OUT GUIDE TUBE OF TAILCONE RELEASE CABLE SYSTEM RH LOWER SECTION. REPLACED GUIDE TUBE IAW AMM 20-30-01-201.SDR DLM88091034Pin · corrodedRUSTED GUARD PINS AND HARDWARE ON TAILCONE RELEASE CONTROL CABLES. GUARD PINS WERE REPLACED IAW AMM 20-30-01-201.SDR DLM88091033Block · wornWORN OUT BLOCK ON TAILCONE RELEASE CABLE SYSTEM AT 2HS POSITION. WORN BLOCKS WERE REPLACED IAW AMM 53-53-00-201.SDR DLM88091031Fitting · crackedCRACKED FITTING TO ATTACH TAILCONE RT UPPER POSITION. REPAIR PIECES WERE FABRICATED IAW DRAWING 9911959 ITEM 43 REV AV AND INSTALLED IAW DRAWING 9911957 REV AV.SDR ASAA0945515Frame · damagedRT FAIRING FORMER HAS ELONGATED HOLES FAIRING FORMER REPLACED.SDR VNAA2009050600001Radome · damagedCREW REPORTED A LIGHTNING STRIKE ON RADOME OF AIRCRAFT IN CLT. MAINTENANCE TESTED, REMOVED AND REPLACED THE RADOME, WEATHER RADAR ANT, TCAS ANT, NR 2 VHF ANT, AND STATIC WICKS ON ELEVATOR. WORK WAS DONE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASSDR CA090501003Radome · damaged(CAN) THE RADOME AND THE LT HORIZONTAL STABILIZER TIP FAIRING. SUFFERED LIGHTNING STRIKE DAMAGE ISSUED REO 690-51-00-036 (FERRY FLIGHT DISPOSITION FOR LIGHTNING STRIKE DAMAGE ON ACFT STRUCTURE).SDR Q2SA746011Fairing · inflt separationON POST-FLIGHT INSPECTION, FOUND SECTION 44 UPPER RT WING-TO-BODY FAIRING PANEL (NR 292DR) MISSING, WITH BROKEN ATTACH BRACKETS ON ACFT STRUCTURE. REPLACED DAMAGED PANEL AND SUPPORT BRACKETS IN ACCORDANCE WITH B747 SRM 51-30-02 AND 51-20-01.SDR IPXA09M55495Radome · damagedINSPECTION TYPE:N/A AT 1500 TO 2000 MSL A/C PASSED THROUGH LARGE FLOCK OF BIRDS. TOOK MULTIPLE HITS, NO IMMEDIATE DAMAGE NOTED. A/C RETURNED TO AIRPORT NORMALLY. NO EMERGENCY. PERFORMED BIRD STRIKE INSPECTION PER AMM 72-00-02-6. NOSE RADOME DAMAGE FROM BISDR QXEA2009040600223Panel · corrodedPDX - C1 - DORSAL FAIRING HAS BLACK STREAKING ON EITHER SIDE AT AFT END OF FAIRING AT BASE OF VERTICAL STAB. REMOVED FLEX JOINT PANELS ON BOTH SIDES OF DORSAL FAIRING AND CLEANED AREA. FOUND FRETTING ON BOTH FLEX JOINT PANELS, BLENDED FRETTING ON LT PANEL ANSDR FDEA200904021138Splice · corrodedWING-TO-BODY FAIRING SPLICE SECTION HAS CORROSION AT STA 800 BL 0. CORROSION ON SPLICE SECTION AT STA 900 BL0, FOUND EXCEEDED SRM ALLOWABLE DAMAGE LIMITS. SPLICE SECTION REMOVED AND REPLACED IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR IAW GMMSDR DLM88090557Mechanism · corrodedDURING HMV RUSTED HARDWARE WAS FOUND ON TAIL RELEASE MECHANISM. REPLACE HARDWARE IAW AMM 20-30-01-201.SDR DLM88090555Guide · wornDURING HMV WEAR WAS FOUND ON CABLE GUIDE TUBE OF TAIL CONE RELEASE SYSTEM. CABLE GUIDE TUBE WAS REPLACE IAW AMM 20-12-01-201.SDR FDEA200903271078Panel · delaminatedFOUND OLD REPAIR ON RT BODY FAIRING PANEL 677GT, C 54.2-55, IN BAD CONDITION. REPAIR RENEWED IAW RAS 70517631/004/2008 ISS B, APPROVED BY EA 6-5350-120215.SDR DLM88090404Sleeve · wornDURING HMV WEAR WAS FOUND ON TAILCONE RELEASE SYSTEM CONTROL CABLE SLEEVE AT Y=1510 BTW 5:00 TO 7:00 O'CLOCK POSITION TAILCONE RELEASE SYSTEM CONTROL CABLE SLEEVE WAS REPLACED IAW MM 20-30-01.SDR USAA2009031090551Fairing · corrodedBFM - C1 - MAJOR REPAIR - SEVERAL SPOTS OF CORROSION ON FUSELAGE LOWER SECTION BELLY FAIRING AT FR44. REPAIRED FUSELAGE LOWER SECTION BELLY FAIRING AT FR44 IAW A330 SRM 51-42-11.SDR DLM88090593Cable · wornWEAR ON CABLE GUIDE TUBE OF TAILCONE RELEASE SYSTEM STA Y=1510. CABLE REPLACED IAW AMM 20-12-01-201.SDR DLM88090586Rod End · corrodedRUSTED CABLE ROD ENDS ON CABLE RELEASE MECHANISM. CABLE REPLACED IAW AMM 53-53-00-501 AND OPS CHECKED ON OPN 8908AD CARD 1141.SDR ASAA0944556Support Angle · crackedUPPER AFT SUPPORT ANGLE CRACKED (WING TO BODY FAIRING SUPPORTS) BS 540 LT SIDE OF RAM AIR INLET. REMOVED DAMAGED SECTION, FABRICATED SPLICE PARTS.SDR ASAA0944555Support Angle · crackedUPPER AFT SUPPORT ANGLE CRACKED (WING TO BODY FAIRING SUPPORTS) RT SIDE OF RAM AIR INLET. REMOVED DAMAGED SECTION, FABRICATED SPLICE PARTS.SDR DLM88090588Mechanism · corrodedRUSTED HARDWARE OF TAILCONE RELEASE MECHANISM STA Y=1510. REPLACED HARDWARE IAW AMM 20-30-01-201.SDR 2009F00021Radome · damagedWHILE UNDERGOING A PREFLIGHT INSP, THE ACFT HIT WITH A HIGH WIND GUST, CAUSING THE ACFT TO SPIN. THE RADOME HIT A MX VAN PARKED ABOUT 10 FEET AWAY, RESULTING IN DAMAGE TO THE RADOME ASSY.SDR WRLA2009039Support Bracket · crackedDURING C-CHECK IN TPE INSPECTION FOUND RT FUSELAGE BODY FAIRING 154GB PANEL SUPPORT BRACKET CRACKED AT STA 1521. REPLACED WITH NEW FABRICATED PART IAW EGAT EI NO W2009P53B-081 REV 0.SDR C77A200005Tail Cone · damagedAIRCRAFT HAD A HARD LANDING IN EWR AND THE TAIL STRUCK THE GROUND. FOUND A 4 FOOT LONG SCRAPE IN THE LOWER SKIN OF THE TAIL CONE WITH THROUGH DAMAGE. AIRCRAFT WAS INSPECTED FOR THE HARD LANDING AND NO FURTHER DAMAGE WAS NOTED.SDR DLM88090257Latch · wornWORN UPPER RT LATCH ON TAILCONE RELEASE SYSTEM. REPLACED LATCH IAW AMM 20-30-01. OPS CHECK WILL BE PERFORMED IAW OPN 7915 CARD 986.SDR ASAA0954290Fairing · chafedWING TO BODY FAIRING DAMAGE 193AR CHAFFED THROUGH. REPAIRED PER SRM 51 70 05.SDR UPS09554582Tail Cone · dentedINSPECTION TYPE:C3 DENT IN FUSELAGE SKIN (TAIL CONE) BS 1989 RT SIDE JUST FWD OF THE APU EXHAUST SHROUD. REPAIRED PER SRM 51-70-10-2R-2 AND AMM 51-21-7.SDR SWIA200921443Strap · corrodedC-CHECK, AFT WING TO FUSELAGE FAIRING STRAP CORRODED. REPAIRED PER SRM.SDR UALA2009012200246Frame · damagedPANEL 191AL DAMAGE, WTB FAIRING STRUCTURE FRAME LOWER CHORD AT STA 987.35 IS BENT & HAS TWO PULLED FASTENERS AT THE L/E INBOARD MOST LATCH LOCATION. SEAL RETAINER IN AREA IS ALSO DAMAGED. INSTALLED FWD HINGE ON NEW REPLACEMENT PANEL 191AL. NEEDS OTHER TWO HSDR DLM88090258Cable · corrodedRUSTED CABLE TERMINALS ON TAILCONE RELEASE SYSTEM. CABLE WAS REPLACED IAW AMM 53-53-00-501. FUNCTIONAL CHECK WILL BE PERFORMED ON OPN 6908AD CARDS 1162 AND 1163.SDR UIEA201000167Fairing · damagedDURING WALKAROUND INSPECTION DAMAGE WAS FOUND TO THE LT WING TO BODY FAIRING 191AHL MEASURING APPROX 12.0 IN X 12.0 IN. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL. "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 44SDR 2009FA0000009Fairing · crackedAIR CONDITIONER CONDENSER L/E FAIRING WAS CRACKED ALL THE WAY ACROSS. THE CRACK RAN THE ENTIRE WIDTH OF THE FAIRING THROUGH THE MOUNTING SCREW HOLES. THE ONLY THING HOLDING IT ON WAS THE CONDENSER ACTUATOR ROD.SDR 2009FA0000054Radome · damagedWHILE PARKED, FBO PERSONNEL BACKED EQUIPMENT INTO NOSE OF AIRCRAFT FWD OF PRESSURE BULKHEAD. DAMAGE TO RADOME, PITOT TUBE, AND SKIN. AIRCRAFT WAS AUTHORIZED FOR SPECIAL FLIGHT PERMIT AND FERRIED TO THE REPAIR STATION. ADDITIONAL INFORMATION AS REPAIRS PROGRSDR DLM88090131Control Cable · brokenBROKEN CONTROL CABLE ASSY OF RELEASE HANDLE TO JETTISON TAIL CONE, REPLACED CABLE.SDR COEA2009010901899Fairing · brokenBODY FAIRING LOST IN FLIGHT: POST FLIGHT INSP, THE RT MLG LEG TO FUSELAGE FAIRING WAS DISCOVERED BROKEN WITH A PORTION OF IT MISSING. REPLACED RT BODY FAIRING.SDR ZZDA2008187Ball · dislodgedTAIL CONE UNLOCK ALERT IN FLIGHT. FOUND INSIDE BALL ON CABLE TO TAIL CONE SWITCH DISLODGED. REINSTALLED CABLE, LIGHT EXTINGUISHED IN COCKPIT. NO OTHER DISCREPANCIES NOTED PER MM 52-73-01 & 53-52-01.SDR C2XA08SH158Panel · corrodedSHV DURING C-CHECK PANEL 191EL WAS FOUND TO HAVE CORRODED BONDING PLATES. MX R&R BONDING PLATES ON PANEL 191EL IAW EC 5750-01315 REV "E". THE ACFT WAS APPROVED TO RETURN TO SERVICE.SDR RMXA0329121708Fairing · delaminatedDURING A SCHEDULED INSP, FOUND THE TAIL ROTOR DRIVESHAFT FAIRING HAS A DELAMINATED AREA ON THE TOP SURFACE. THE DELAMINATED AREA WAS 8 INCHES L X 2.25 INCHES W. REPAIR SCHEME WAS PROVIDED FROM THE MFG AND THE FAIRING WAS REPAIRED.SDR M7KA1017084173Latch · wornDURING ROUTINE INSP, LATCH APPEARED LOOSE AND CLOSER INSPECTION REVEALED LOCKING LATCH HINGE PINS SOCKETS AND HOOK CATCH WORN EXCESSIVELY. INSTALLED NEW LATCHES AS REQUIRED.SDR M7KA1028084248Latch · wornDURING ROUTINE INSPECTION LATCH APPEARED LOOSE AND CLOSER INSPECTION REVEALED LOCKING LATCH HINGE PINS SOCKETS AND HOOK CATCH WORN EXCESSIVELY. HINGE ATTACHMENT BORE HAD A 1` LONG CRACK RADIATING. INSTALLED NEW LATCHES AS REQUIRED.SDR VNAA2008111900004Radome · damagedCREW REPORTED THE AIRCRAFT EXPERIENCED STATIC DISCHARGE FROM THE FRONT RIGHT, WHICH WAS VISIBLE AND AUDIBLE FROM THE COCKPIT WHILE FLYING THROUGH A RAIN SHOWER. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT WINGLET, THE RIGHT SIDE OF THE FUSELAGE AND THSDR HALA2008111300847Support Angle · corrodedFAIRING 139C SUPPORTING CROSSMEMBER CORRODED AROUND SWAGE NUTS, CROSSMEMBER (P/N:145T8629-2). REPLACED, PAINT AND CPC APPLICATION PRIOR TO RE-INSTALLATION.SDR DL757081468Support · corrodedWHILE WORKING CUSTOMER CARD 00068 FOUND FAIRING SUPPORT STRUCTURE CRACKED AT BS 780-800 BL 0. REMOVED AND REPLACED FAIRING SUPPORT STRUCTURE BS 780-800 BL 0 IAW SRM 51-40-02.SDR 08FDEA04561Frame · crackedTAIL CONE RIGHT FRAME HAS A CRACK WITH A PREVIOUS STOP DRILL HOLE AT STA 2199 AT THE UPPER LONGERON. FORMED ANGLE PER SRM 53-30-00. FABBED, LOCATED, & DRILLED HOLES PER SRM 53-30-00. ALODINED & PRIMED PER SRM 51-21-01. INSTALLED PER SRM 51-35-01.SDR QXEA2008111201153Fairing · chafedPDX - C1 - FUSELAGE FAIRING PANEL 261FT HAS CHAFING ALONG FWD EDGE UNDERSIDE MATING EDGE. BLENDED OUT DAMAGE MAX MATERIAL REMOVED .003" IAW RD 8/4-53-521 STEP 1-2. HFEC INSPECTED AREA IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ALODINED AND PRIMED AREASDR QXEA2008111201152Fairing · chafedPDX - C1 - FUSELAGE FAIRING PANEL 261CT HAS CHAFING ALONG FWD EDGE UNDERSIDE MATING SURFACE. BLENDED DAMAGED AREA MAX MATERIAL REMOVED .003" , IAW RD 8/4-53-521 STEP 1-2. HFEC AREA IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ALODINED AND PRIMED REPAIR SDR 08FDEA04535Frame · gougedTAIL CONE RIGHT UPPER FRAME IS GOUGED, 3 PLACES. REMOVED RIGHT UPPER SUPPORT PER DC/MD-10 SRM 51-35-01; VOL II. FABRICATED, LOCATED AND DRILLED HOLES PER DAC DWG AKC7068; REV "T". INSTALLED SUPPORT PER DC/MD-10 SRM 51-33-01; VOL II AND DC/MD-10 SRM 51-35-
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